IRIDIUM 106, 41917
Orbit data source: Space-Track
IRIDIUM 106, 41917 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 14 Jan 2017 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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41917 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
OATK SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 IRIDIUM 106
1 41917U 17003A 26040.27956249 -.00000023 00000-0 -15192-4 0 9998
2 41917 86.4022 142.0223 0001674 91.0655 269.0733 14.34217461474877Epoch: 2026-02-09T06:42Z
TLE epoch observation values (Epoch: 2026-02-09T06:42:34.199Z)
Latitude
0.00004°
Longitude
-97.99685°
Altitude
780.739 km
Speed
7.463 km/s
True Right ascension
09h 28m 05s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
13:57:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.83 km
Perigee altitude
773.435 km
Semi-major axis
7,152.769 km
Eccentricity
0.00017
Inclination
86.4022°
RAAN
142.0223°
Arg. of periapsis
91.0655°
True anomaly
269.05412°
Mean anomaly
269.0733°
Eccentric anomaly
269.06371°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.000015192
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Other satellites on launch #3 in the year 2017 (2017-01-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IRIDIUM 106 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-02-09 19:01:33.390Z | 351.287° N | 2026-02-09 19:04:33.390Z | 303.442° NW | 43.564° | 2026-02-09 19:09:33.390Z | 185.989° SSW |
| 7 mins | 2026-02-10 06:17:33.390Z | 125.442° SE | 2026-02-10 06:20:33.390Z | 79.355° E | 23.203° | 2026-02-10 06:24:33.390Z | 28.492° NE |
| 8 mins | 2026-02-10 07:57:33.390Z | 222.592° SW | 2026-02-10 08:00:33.390Z | 269.956° W | 29.106° | 2026-02-10 08:05:33.390Z | 343.531° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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